Tire pressure indicator
US-2015231936-A1 · Aug 20, 2015 · US
US9845163B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9845163-B2 |
| Application number | US-201615297409-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 19, 2016 |
| Priority date | Oct 20, 2015 |
| Publication date | Dec 19, 2017 |
| Grant date | Dec 19, 2017 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A display assembly for displaying a parameter of an aircraft, comprising a parameter device and a non-transparent display device. The parameter device for gathering a parameter of the aircraft and/or of an equipment of the aircraft includes a sending unit for sending the parameter. The non-transparent display device is detachable, is configured to display the parameter, and comprises a receiving unit for receiving the parameter. The sending unit transmits the parameter directly to the receiving unit.
Opening claim text (preview).
The invention claimed is: 1. A display assembly for displaying a parameter of an aircraft, comprising: a parameter device for gathering a parameter of at least one of the aircraft or an equipment of the aircraft, including a sending unit for sending the parameter; and a detachable non-transparent display device, configured to display the parameter, and comprising a receiving unit for receiving the parameter; a work clothing for an operator of the aircraft to which the display device is attached, a plurality of display components arranged at different positions of the work clothing and the aircraft so that a display for the parameter is always in a field of view of a pilot or the operator; wherein the sending unit is configured to transmit the parameter directly to the receiving unit. 2. The display assembly according to claim 1 , wherein the display device comprises a hand-held component. 3. The display assembly according to claim 1 , wherein the display device comprises an attachment portion configured for attaching the display device to a work clothing of an operator of the aircraft. 4. The display assembly according to claim 1 , wherein the display device comprises an illumination component that is selectively illuminated if the parameter is in a predetermined range. 5. The display assembly according to claim 4 , wherein the illumination component includes one or more light emitting diodes. 6. The display assembly according to claim 1 , wherein the display device comprises a display component that displays the parameter. 7. The display assembly according to claim 6 , wherein the display component includes a liquid crystal display. 8. The display assembly according to claim 1 , the sending unit comprising a wireless transmitter, wherein the parameter is wirelessly transmitted between the sending unit and the receiving unit. 9. The display assembly according to claim 1 , wherein the parameter device and the display device are arranged in a single component, wherein preferably the parameter device comprises a sensor for measuring the parameter. 10. An aircraft assembly, comprising: an aircraft and a display assembly for displaying a parameter of the aircraft, comprising: a parameter device for gathering a parameter of at least one of the aircraft or an equipment of the aircraft, including a sending unit for sending the parameter; and a detachable non-transparent display device, configured to display the parameter, and comprising a receiving unit for receiving the parameter; a work clothing for an operator of the aircraft to which the display device is attached, a plurality of display components arranged at different positions of the work clothing and the aircraft so that a display for the parameter is always in a field of view of a pilot or the operator; wherein the sending unit is configured to transmit the parameter directly to the receiving unit. 11. The aircraft assembly according to claim 10 , wherein the aircraft is a helicopter having a skid. 12. The aircraft assembly according to claim 11 , wherein the display device is attached to the skid. 13. An aircraft assembly, comprising: an aircraft; a winch configured to raise and lower a cable; a controller for controlling the winch and comprising a hand-held unit; a display assembly for displaying a parameter of the aircraft, comprising: a parameter device for gathering a parameter of at least one of the aircraft or an equipment of the aircraft, including a sending unit for sending the parameter; and a detachable non-transparent display device, configured to display the parameter, and comprising a receiving unit for receiving the parameter; a work clothing for an operator of the aircraft to which the display device is attached, a plurality of display components arranged at different positions of the work clothing and the aircraft so that a display for the parameter is always in a field of view of a pilot or the operator; wherein the sending unit is configured to transmit the parameter directly to the receiving unit.
specially adapted for helicopters · CPC title
Aircraft indicators or protectors not otherwise provided for · CPC title
Flight suits · CPC title
Arrangements or adaptations of instruments · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.